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Volumn 20, Issue 3, 2006, Pages 500-506

Thermal shielding of a reentry vehicle by ultra-high-temperature ceramic materials

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CERAMIC MATERIALS; FUSELAGES; HEAT SHIELDING; MANEUVERABILITY; NUMERICAL ANALYSIS; WINGS;

EID: 33747053695     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/1.17947     Document Type: Article
Times cited : (31)

References (12)
  • 1
    • 9144256693 scopus 로고    scopus 로고
    • A new philosophy for the design of reentry vehicles
    • Monti, R., and Pezzella, G., "A New Philosophy for the Design of Reentry Vehicles," Space Technology, Vol. 24, No. 4, 2004, pp. 179-191.
    • (2004) Space Technology , vol.24 , Issue.4 , pp. 179-191
    • Monti, R.1    Pezzella, G.2
  • 3
    • 33747070538 scopus 로고    scopus 로고
    • SHARP: NASA's research and development activities in ultra high temperature ceramic nose caps and leading edges for future space transportation vehicles
    • Paper IAF-01-V5.02, Toulouse, France, Oct.
    • Arnold, J., Johnson, S., and Wercinski, P., "SHARP: NASA's Research and Development Activities in Ultra High Temperature Ceramic Nose Caps and Leading Edges for Future Space Transportation Vehicles," Paper IAF-01-V5.02, IAF Symposium, Toulouse, France, Oct. 2001.
    • (2001) IAF Symposium
    • Arnold, J.1    Johnson, S.2    Wercinski, P.3
  • 4
    • 33644770400 scopus 로고    scopus 로고
    • NSF-AFOSR joint workshop on future ultra-high temperature materials
    • URL: web.umr.edu/~uhtm [cited 11 Jan. 2005]
    • Fahrenoltz, W. G., Hilmas, G. E., "NSF-AFOSR Joint Workshop on Future Ultra-High Temperature Materials," Final Rept., 2004, URL: web.umr.edu/~uhtm [cited 11 Jan. 2005].
    • (2004) Final Rept.
    • Fahrenoltz, W.G.1    Hilmas, G.E.2
  • 6
    • 29044433434 scopus 로고
    • Shuttle performance: Lessons learned
    • Arringhton, J. P., Jones, J. J., "Shuttle Performance: Lessons Learned," NASA CP-2283, Pt. 1, 1983, pp. 473-508.
    • (1983) NASA CP-2283 , Issue.1 PART , pp. 473-508
    • Arringhton, J.P.1    Jones, J.J.2
  • 7
    • 0024703034 scopus 로고
    • A review of high speed convective, heat-transfer computation methods
    • July
    • Tauber, M. E., "A Review of High Speed Convective, Heat-Transfer Computation Methods," NASA TP 2914, July 1989.
    • (1989) NASA TP , vol.2914
    • Tauber, M.E.1
  • 9
    • 84888833857 scopus 로고    scopus 로고
    • NASA Ames Research Center, [cited 15 Feb. 2005]
    • "TPS-X Database," NASA Ames Research Center, http://tpsx.arc.nasa. gov [cited 15 Feb. 2005].
    • TPS-X Database
  • 10
    • 4544273437 scopus 로고    scopus 로고
    • Processing, properties and arc-jet oxidation of hafnium diboride/silicon carbide ultra high temperature ceramics
    • Gasch, M., Ellerby, D., Irby, E., Beckman, S., Gusman, M., and Johnson, S., "Processing, Properties and Arc-Jet Oxidation of Hafnium Diboride/Silicon Carbide Ultra High Temperature Ceramics," Journal of Materials Science, Vol. 39, No. 19, 2004, pp. 5925-5937.
    • (2004) Journal of Materials Science , vol.39 , Issue.19 , pp. 5925-5937
    • Gasch, M.1    Ellerby, D.2    Irby, E.3    Beckman, S.4    Gusman, M.5    Johnson, S.6
  • 11
    • 29044444992 scopus 로고    scopus 로고
    • On wind tunnel testing of low risk re-entry trajectory
    • 4th International Symposium Atmospheric Reentry Vehicles and Systems, AAAF, Arcachon, France, March
    • Monti, R., Savino, R., and De Stefano Fumo, M., "On Wind Tunnel Testing of Low Risk Re-entry Trajectory," 4th International Symposium Atmospheric Reentry Vehicles and Systems, 4th International Symposium Atmospheric Reentry Vehicles and Systems, AAAF, Arcachon, France, March 2005.
    • (2005) 4th International Symposium Atmospheric Reentry Vehicles and Systems
    • Monti, R.1    Savino, R.2    De Stefano Fumo, M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.